System employed in development of Navy's supersonic F11F-1 airplane; objective was to provide reliable, light weight, automatic method of close center of gravity travel independent of electric power; aim achieved through use of hydromechanical devices which utilize compressor bleed air from jet engine as muscle force; advantages.


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    Titel :

    Fuel balance system for supersonic airplanes


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:
    Karanik, J. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1956 Supersonic speeds



    Erscheinungsdatum :

    1956


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Fuel balance system for supersonic airplanes

    Karanik, J. | Engineering Index Backfile | 1957


    FUEL BALANCE SYSTEM FOR SUPERSONIC AIRPLANES

    KARANIK, JOHN | SAE Technical Papers | 1956


    Thrust Requirements for Supersonic Airplanes

    P. G. Thome / H. E. Nicoll | NTIS | 1960


    Optimal cruise trajectories for supersonic airplanes

    Teren, Fred / Daniele, Carl J. | TIBKAT | 1972


    Optimal cruise trajectories for supersonic airplanes

    Teren, F. / Daniele, C. J. | NTRS | 1972